EP0360376A2 - Firing circuit for a vehicle passenger restraint system - Google Patents
Firing circuit for a vehicle passenger restraint system Download PDFInfo
- Publication number
- EP0360376A2 EP0360376A2 EP89304475A EP89304475A EP0360376A2 EP 0360376 A2 EP0360376 A2 EP 0360376A2 EP 89304475 A EP89304475 A EP 89304475A EP 89304475 A EP89304475 A EP 89304475A EP 0360376 A2 EP0360376 A2 EP 0360376A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- circuit
- voltage
- junctions
- fault
- leg
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000010304 firing Methods 0.000 title claims abstract description 85
- 239000003990 capacitor Substances 0.000 claims description 12
- 238000003745 diagnosis Methods 0.000 claims description 4
- 230000011664 signaling Effects 0.000 claims description 3
- 230000001133 acceleration Effects 0.000 description 10
- 238000000034 method Methods 0.000 description 5
- 230000007257 malfunction Effects 0.000 description 3
- 230000004069 differentiation Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 238000010926 purge Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R21/00—Arrangements or fittings on vehicles for protecting or preventing injuries to occupants or pedestrians in case of accidents or other traffic risks
- B60R21/02—Occupant safety arrangements or fittings, e.g. crash pads
- B60R21/16—Inflatable occupant restraints or confinements designed to inflate upon impact or impending impact, e.g. air bags
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R21/00—Arrangements or fittings on vehicles for protecting or preventing injuries to occupants or pedestrians in case of accidents or other traffic risks
- B60R21/01—Electrical circuits for triggering passive safety arrangements, e.g. airbags, safety belt tighteners, in case of vehicle accidents or impending vehicle accidents
- B60R21/017—Electrical circuits for triggering passive safety arrangements, e.g. airbags, safety belt tighteners, in case of vehicle accidents or impending vehicle accidents including arrangements for providing electric power to safety arrangements or their actuating means, e.g. to pyrotechnic fuses or electro-mechanic valves
- B60R21/0173—Diagnostic or recording means therefor
- B60R21/0176—Diagnostic or recording means therefor for firing circuits using only mechanical switches as collision detecting means, in series with pyrotechnic fuses
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R21/00—Arrangements or fittings on vehicles for protecting or preventing injuries to occupants or pedestrians in case of accidents or other traffic risks
- B60R21/02—Occupant safety arrangements or fittings, e.g. crash pads
- B60R21/06—Safety nets, transparent sheets, curtains, or the like, e.g. between occupants and glass
- B60R21/08—Safety nets, transparent sheets, curtains, or the like, e.g. between occupants and glass automatically movable from an inoperative to an operative position, e.g. in a collision
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B9/00—Safety arrangements
- G05B9/02—Safety arrangements electric
- G05B9/03—Safety arrangements electric with multiple-channel loop, i.e. redundant control systems
Definitions
- the instant invention relates to vehicle passenger restraint systems and, more specifically, to a firing circuit for an air bag passive restraint system which can be readily diagnosed for the presence of faults therein.
- Known air bag passenger restraint systems comprise a firing circuit having a voltage supply providing a potential across a firing squib in series with a first and second normally open vehicle acceleration sensor, each of which is shunted by a resistor of like nominal resistance. A small current thus flows through the circuit while the sensors remain in the normally open condition. The closure of the sensors upon collision or marked deceleration of the vehicle generates a significant rise in the current flowing through the squib which, in turn, fires the squib to deploy the air bag.
- a separate firing circuit is employed for each air bag, each firing independently during a vehicle collision.
- Another known air bag firing circuit offers multiple firing paths by placing in series a first pair of normally open sensors wired in parallel, a pair of squibs wired in parallel, and a second pair of normally open sensors, also wired in parallel.
- the sensors are again shunted by resistors of like nominal resistance.
- the squibs fire upon simultaneous closure of either of the first pair of sensors and either of the second pair of sensors.
- the provision of multiple firing paths thus increases system reliability without the need for increasing the number of circuit elements used therein.
- Unfortunately such circuits are not readily diagnosable--although the examination of voltage potentials about the circuit would indicate that a fault had occurred, there is no way to identify the precise fault, short of removing and testing each circuit element individually until the source of the fault is revealed. For example, upon the failing closed of one of the sensors comprising the first pair of sensors, both sensors must be removed and individually tested to determine which of the sensors had failed.
- Another object of the instant invention is to provide a firing circuit for a vehicle passenger restraint system, the elements of which may be diagnosed without necessitating the disassembly of the firing circuit.
- a further object of the instant invention is to provide a method for specifically diagnosing any fault present in the instant firing circuit which does not require the disassembly thereof.
- the instant firing circuit for actuating a first and second instrumentality of a vehicle passenger restraint system comprises first and second circuit legs connected in parallel across a voltage supply, whereby a first voltage is applied thereacross.
- the first circuit leg comprises in series a first normally open sensor for detecting a first condition requiring deployment of the air bags (hereinafter "safing sensor”), a first trigger means such as a squib for deploying the first air bag having an internal resistance, and a second normally open sensor for detecting a second condition requiring deployment of the air bags (hereinafter "crash sensor").
- the second circuit leg comprises in series another safing sensor, a second squib for deploying the second air bag having an internal resistance substantially equal to the internal resistance of the first squib, and another crash sensor.
- Each of the normally open safing and crash sensors are shunted by a resistor having a resistance substantially greater than the internal resistance of each squib.
- the resistors shunting the crash and safing sensor of the first and second circuit legs, respectively, are of like nominal resistance.
- the resistors shunting the safing sensor of each circuit leg, and the resistors shunting the crash sensor of each circuit leg, respectively are of like nominal resistance.
- a first diode bridge comprising a pair of oppositely biased diodes connects a first junction on the first circuit leg located between the safing sensor and the squib thereof with a first junction on the second circuit leg located between the safing sensor and squib thereof.
- a second diode bridge comprising a pair of oppositely biased diodes connects a second junction on the first circuit leg located between the squib and crash sensor thereof with a second junction on the second circuit leg located between the squib and crash sensor thereof.
- the diode bridges provide multiple firing paths for the squibs, whereby both squibs are fired and, hence, both air bags are deployed, upon closure of either safing sensor and either crash sensor.
- the diode bridges additionally permit the diagnosing of the presence of a fault in the instant firing circuit in situ, as well as permitting the identification of the fault.
- the instant firing circuit further comprises means for reading the voltage potentials at several of the junctions thereabout and the voltage applied across the circuit legs; means for comparing the voltage potentials of the several junctions with each other; means for calculating a plurality of voltage ranges from the applied voltage and a plurality of known percentages of the applied voltage, and means for comparing the voltage potential at one of the junctions with the thus calculated voltage ranges; means for applying a second voltage across the circuit legs greater than the first applied voltage, i.e., for increasing the voltage applied thereacross, and means for comparing the voltage potential at one of the junctions upon application of the first voltage across the circuit legs with the voltage potential at the same junction when the second voltage is applied thereacross; and means for comparing the voltage drop across each of the diode bridges with the diode forward-biased conduction voltages.
- the instant firing circuit further comprises signal means for signalling the presence of the fault, and means for recording the fault, upon the diagnosis thereof. Additionally, the instant firing circuit comprises means for determining the instantaneous forward-biased conduction voltages of the diodes comprising the diode bridges, such as switchable means for drawing current from each of the circuit legs and means for calculating the resultant voltage drop across each of the diode bridges, whereby the firing circuit periodically redetermines the forward-biased conduction voltage of the diodes so as to account for manufacturing tolerances as well as the effects of time and temperature thereon.
- a firing circuit 10 constructed in accordance with the instant invention for deploying a pair of air bags (not shown) comprises a first and second circuit leg 12 and 14 connected in parallel across a DC power supply 16.
- the DC power supply 16 comprises, for example, a battery 18 and a capacitor 20 connected across the battery 18 and normally charged thereby, whereby the supply voltage V s delivered across the circuit legs 12 and 14 remains sufficient to deploy the air bags in the event that the battery 18 malfunctions or is otherwise isolated from legs 12 and 14 of the firing circuit 10 during a vehicle collision.
- the capacitor 20 is charged to the nominal supply voltage V s by the pulsed output of a charging transistor 22 with the aid of an inductor 24.
- the input to the charging transistor 22 comprises the pulsed output of a microprocessor 30 which continuously monitors the output voltage V bat of the battery 18 and the supply voltage V s applied across the circuit legs 12 and 14 by means of a pair of analog-to-digital converter ports A and B thereon, respectively.
- a pair of protecting diodes 32 prevent the premature discharge of the capacitor 20. It is noted that the capacitor 20 further serves to momentarily increase the supply voltage V s applied across the legs 12 and 14 of the firing circuit 10 for use in diagnosing the presence of faults therein, as described hereinbelow.
- the first circuit leg 12 comprises in series a normally open safing sensor 34 for detecting a first condition requiring the deployment of the air bags, such as an acceleration which exceeds a first threshold value; a trigger means for deployment of the first air bag, such as a firing squib 36 therefor comprising a heating wire of nominal internal resistance which explosively deploys the first air bag when the current flowing therethrough exceeds a threshold value; and a normally open crash sensor 38 for detecting a second condition requiring the deployment of the air bags, such as an acceleration which exceeds a second threshold value.
- a normally open safing sensor 34 for detecting a first condition requiring the deployment of the air bags, such as an acceleration which exceeds a first threshold value
- a trigger means for deployment of the first air bag such as a firing squib 36 therefor comprising a heating wire of nominal internal resistance which explosively deploys the first air bag when the current flowing therethrough exceeds a threshold value
- a normally open crash sensor 38 for detecting a second condition
- the second acceleration threshold of the crash sensor 38 is higher than the first acceleration threshold of the safing sensor 34, whereby the safing sensor 34 effectively "arms” the crash sensor 38, and the thus armed crash sensor 38 fires the squib 36 upon the acceleration of the vehicle at a rate which exceeds the second threshold value thereof.
- the normally open sensors 34 and 38 of the first circuit leg 12 are each shunted by a resistor 40 of like nominal resistance.
- the nominal resistance of the shunting resistors 40 is preferably several orders of magnitude larger than the nominal internal resistance of the squib 36.
- the shunting resistors 40 preferably comprise 2k resistors.
- the second leg 14 of the firing circuit 10 comprises in series a second safing sensor 42 having a like acceleration threshold as the safing sensor 34 of the first circuit leg 12; a second squib 44 having a like internal resistance as that of the first squib 36 for deployment of the second air bag when the current flowing there through exceeds a threshold value; and a second crash sensor 46 having a like acceleration threshold as the crash sensor 38 of the first circuit leg 12.
- the safing sensor 42 and the crash sensor 46 of the second circuit leg 14 are each shunted by a resistor 48 of like nominal resistance as the shunting resistors 40 of the first circuit leg 12.
- a first diode bridge 50 comprising oppositely biased diodes 52 connects a junction 54 on the first leg 12 between the safing sensor 34 and the squib 36 thereof (hereinafter the "first junction 54") with a junction 56 on the second leg 14 between the safing sensor 42 and the squib 44 thereof (hereinafter the "second junction 56").
- a second diode bridge 60 comprising oppositely biased diodes 62 connects another junction 64 on the first circuit leg 12 between the squib 36 and the crash sensor 38 thereof (hereinafter the "third junction 64") with another junction 66 on the second circuit leg 14 between the squib 44 and the crash sensor 46 thereof (hereinafter the "fourth junction 66").
- the diode bridges 50 and 60 provide multiple firing paths for the squibs 36 and 44, whereby both air bags are deployed regardless of which combination of safing sensor and crash sensor closures occur. More specifically, under normal operation, the shunting resistors 40 and 48 maintain a relatively low current flow through each circuit leg 12 and 14, and, hence, through the squibs 36 and 44 thereof. Upon the closure of at least one of the safing sensors 34 and 42 and at least one of the crash sensors 38 and 46 due to an acceleration exceeding the threshold values thereof, the shunting resistors 40 and 48 are shorted, whereby the current flowing through both squibs 36 and 44 is increased to a value above the firing threshold thereof, whereupon the air bags are simultaneously deployed.
- the diode bridges 50 and 60 of the instant firing circuit 10 additionally permit the diagnosing of faults therein. More specifically, during normal operation, the firing circuit 10 functions as a simple parallel circuit having two legs 12 and 14 of identical resistance which, hence, draw an identical current. Therefore, during normal operation, the first and second junctions 54 and 56, and the third and fourth junctions 64 and 66, respectively, are maintained at like potentials. However, the presence of a fault within the circuit 10 disrupts the current flow through the legs 12 and 14 thereof, thereby altering the voltage potentials at one or more of the junctions. Since each fault affects the circuit and, hence, the junction voltage potentials in a different manner, the identity of the fault may be determined upon examination of the absolute and relative values of the voltage potentials at the junctions 54, 56, 64, and 66.
- the instant firing circuit 10 further comprises means for reading the voltage potentials at each junction 54, 56, 64, and 66, such as analog-to-digital converter ports "C", “D”, “E”, and “F” on the microprocessor 30 which are connected thereto, respectively.
- the firing circuit 10 further comprises a non-volatile memory unit such as an EEPROM 68 connected with the microprocessor 30 for storing a plurality of reference values useful in diagnosing the presence of faults, and wherein the frequency and identity of such diagnosed faults are recorded for subsequent review; and signal means, such as signal lamp 70, actuated by the microprocessor 30, whereby the presence of a fault is indicated to the vehicle operator.
- the diagnostic sequence executed by the microprocessor 30 is shown schematically in FIG. 2. Specifically, the microprocessor 30 diagnoses the presence, if any, of a fault in the firing circuit 10 by: 1) reading the instantaneous supply voltage V s and the voltage potentials at the junctions 54, 56, 64, and 66 via analog-to-digital converter ports "B", “C”, “D”, “E”, and “F” thereon, respectively; (2) retrieving from the EEPROM 68 a plurality of range percentages previously recorded therein which define ranges of junction voltage potentials with respect to the supply voltage V s corresponding to various groupings of possible circuit faults; (3) calculating five voltage ranges using the above percentages and the instantaneous supply voltage V s ; and (4) determining the presence and identity of any specific fault based on: (a) the voltage range in which the voltage potential V1 at the first junction 54 lies; (b) the voltage drop V12 between the first and second junctions 54 and 56 in comparison with a reference diode forward-biased conduction
- the microprocessor 30 thereafter records the indicated fault in the EEPROM 68 and empowers the signal lamp 70. It is noted that the fault range percentages may be alternately imbedded in the set of instructions to be executed by the microprocessor 30, whereby reference need no longer be made to the EEPROM 68 to obtain such values.
- the fault range percentages retrieved from the EEPROM 68 in step (2) above are initially determined by circuit analysis in a manner known to those skilled in the art, whereby the likely change in voltage potentials at the junctions 54, 56, 64 and 66, respectively, in response to each possible fault is calculated. The percentages thus obtained are then empirically broadened to provide fault voltage ranges which accommodate allowable variations in the electrical characteristics of the elements comprising the firing circuit 10.
- Range 1 lies between ground and 16.5% of the supply voltage V s ; Range 2 between 16.5% and 46% of the supply voltage V s ; Range 3 between 46% and 58% of the supply voltage V s ; Range 4 between 58% and 79% of the supply voltage V s ; and Range 5 between 79% and 100% of the supply voltage V s .
- the above percentages hold true for any embodiment in which the shunting resistors 40 and 48 are of like nominal resistance and the nominal internal resistance of the squibs 36 and 44 is negligible when compared therewith.
- the supply voltage V s is 12 volts and, thus, the Ranges 1-5 as calculated under step (2) above are as follows: Range 1, 0.0 to 1.98 volts; Range 2, 1.98 to 4.86 volts; Range 3, 4.86 to 6.88 volts; Range 4, 6.88 to 9.42 volts; and Range 5, 9.42 to 12.0 volts. It is assumed, for the following examples, that the diode forward-biased conduction voltage V d has been found to be 0.70 volts.
- the voltage potentials at the first, second, third and fourth junctions 54, 56, 64, and 66 are determined to be 12.00, 12.00, 11.98, and 11.99 volts, respectively. Given the 12 volt supply voltage, the first junction potential V1 falls within Range 5. Since the voltage drop V12 between the first and second junctions 54 and 56 is zero, initial reference to Table I using only V12 identifies the following possible fault conditions: both squibs 36 and 44 are open (fault no. 7); both safing sensors 34 and 42 are closed (fault no. 8); the first and second junctions 54 and 56 are both shorted to the positive terminal of the battery 18 (fault no.
- circuit legs 12 and 14 are open between the third junction 64 and ground, and between the fourth junction 66 and ground, respectively, (fault no. 10); or both the third and the fourth junctions 64 and 66 of the firing circuit 10 are shorted to the positive terminal of the battery 18 (fault no. 11).
- the capacitor 20 is charged by turning on charging transistor 22. If such charging produces an increase in the voltage potential at the first junction 54, then reference to Table 1 indicates that both safing sensors 34 and 42 are closed (fault no. 8). If such charging fails to produce an increase in the voltage potential at the first junction 54, then the first and second junctions 54 and 56 are shorted to the battery 18 (fault no. 8).
- the microprocessor 30 can compare the battery voltage V bat with the voltage potential at the first junction V1 via analog-to-digital convertor ports "A" and "C” on the microprocessor 30 that are connected therewith, respectively.
- V bat the battery voltage V bat is substantially equal to the voltage potential at the first junction 54
- the first and second junctions 54 and 56 are shorted to the battery 18, i.e., fault no. 8 is indicated.
- the specific fault in this example cannot be identified. Rather, the fault may only be characterized as being within two groups of faults, namely, either in the group comprising fault nos. 7, 8, and 10, or in the group comprising fault nos. 9 and 11.
- the voltage potentials at the first, second, third and fourth junctions 54, 56, 64, and 66 are determined to be 11.98, 12.00, 11.28, and 11.30 volts, respectively.
- the first junction potential thus falls within Range 5.
- Initial reference to Table I using V12 indicates the following possible fault conditions: the first junction 54 is shorted to the positive terminal of the battery 18 (fault no. 1); the first safing sensor 34 is closed (fault no. 2); or the third junction 64 is shorted to the positive terminal of the battery 18 (fault no. 3).
- Further reference to Table I using the small negative voltage drop V13 present between the first and third junctions 54 and 64 indicates that the first junction 54 is shorted to the positive terminal of the battery 18 (fault no. 1).
- the voltage potentials at the first, second, third and fourth junctions 54, 56, 64, and 66 are determined to be 6.10, 6.10, 6.06, and 6.07, respectively.
- the first junction potential thus falls within Range 3. Since the first and second junctions 54 and 56 are of equal voltage potential, there is no fault present within the circuit 10.
- the voltage potentials of the first, second, third and fourth junctions 54, 56, 64, and 66 are determined to be 5.97, 6.12, 5.93, and 6.10 volts, respectively.
- the first junction potential thus falls within Range 3.
- at least one of the shunting resistors 40 and 48 in the circuit 10 has a nominal resistance outside of the acceptable range therefor (fault no. 17).
- each circuit leg 12 and 14 in between the crash sensor 38 and 46 thereof and ground, further differentiation between the alternate conditions within faults no 21, 23, and 25 may be made. More specifically, the second and fourth junctions 64 and 66 are not shorted to ground where the voltage potentials thereof are equal to the forward-biased conduction voltage V d of such additional resistors. In contrast, a short to ground is indicated where the voltage potentials of the second and fourth junctions 64 and 66 are zero.
- the presence of such additional diodes in the circuit legs 12 and 14 alters the above fault range percentages and, hence, the fault ranges applicable for circuit diagnosis, due to the forward-biased conduction voltage V d thereof.
- a resistor (not shown) having a resistance substantially greater than either of the resistors 40 and 48 shunting the crash sensors 34 and 42 may also shunt each crash sensor 34 and 42, whereby further differentiation between the alternate conditions within fault no 26 may be made.
- the firing circuit 10 of the instant invention further comprises current switch means, such as transistors 72 and 74, connected to the third and fourth junctions 64 and 66, respectively, for selectively drawing current from the circuit legs 12 and 14 thereof, as illustrated in FIG. 1.
- each transistor 72 and 74 is connected to the third and fourth junctions 64 and 66, respectfully, via a resistor 76 of like resistance as the shunting resistors 40 and 48, with the emitter of each transistor 72 and 74 being connected to ground.
- FIG. 3 The method for determining the instantaneous forward-biased conduction voltages V d of the diodes 52 and 62 comprising the diode bridges 50 and 60 is illustrated in FIG. 3. Specifically, a current is supplied to the base of the first transistor 72 from the microprocessor 30, thereby drawing current through the resistor 76 connected to the collectors thereof.
- the above method is repeated with the second transistor 74 drawing current from the second leg 14, whereby the instantaneous forward-biased conduction voltage V d of each of the oppositely-biased diodes 52 and 62 of the bridges 50 and 60 are calculated.
- the instantaneous forward-biased conduction voltage V d of each diode 52 and 62 is thereafter stored in the EEPROM 68 for use in the diagnostic sequence described hereinabove.
- diode forward-biased conduction voltages V d a preselected value for the diode forward-biased conduction voltages V d is used if the instantaneous voltage drop across the diode cannot be calculated due to transistor or diode malfunction.
- the diode forward-biased conduction voltages V d can be accurately checked only when there are no faults present in the firing circuit 10, or when the faults present fall within Range 3, as defined hereinabove.
- the instant diagnostic sequence may additionally comprise the steps of: reading the voltage potentials V12, V13, V23, and V34 about the firing circuit several times and calculating average values therefrom for use the steps outlined hereinabove; checking the integrity of the signal lamp 70 and empowering a back-up signal means in the event of a failure of the signal lamp 70; signaling the specific fault detected, as by a coded sequence, via the signal lamp 70; reading the output voltage V s of the battery 18 via analog-to-digital port "A" on the microprocessor 30 and charging the capacitor 20 if the battery voltage V bat falls below the level sufficient to fire both squibs 36 and 44, as may occur, for example, upon malfunction of the battery 18 or the isolation of the battery 18 from the circuit 10 during a vehicle collision; and verifying the physical attachment of the acceleration sensors 34, 40, 42, and 46 to the vehicle frame through the use of additional sensing means therefor (not shown).
- the microprocessor 30 may incorporate means therein, such as incremental counters, for determining whether the indicated fault is a system aberration, such as a momentary closure of one of the safing sensors 34 and 42, or a true fault, such as a sensor which has failed in the closed position.
- the microprocessor 30 may further incorporate a deadman timer to ensure continued diagnostic capability therein, e.g., to cause the microprocessor 30 to begin at a specific point in the instructions therefor in the event that the microprocessor 30 is tied up by a random external disturbance.
- the microprocessor 30 instructions may further comprise steps for checking the integrity of the EEPROM 68 connected therewith, and for recording in the EEPROM 68 the purging of the faults recorded therein.
- FIG. 4 An alternate embodiment 80 of the instant air bag firing circuit is illustrated in FIG. 4.
- the firing circuit 80 actuates a single air bag, such as a driver's side air bag (not shown), while providing multiple firing paths and full circuit diagnosability.
- the firing circuit 80 comprises three circuit legs 82, 84, and 86 connected in parallel across a voltage supply 16 similar to that described hereinabove with respect to the first embodiment 10 of the instant firing circuit.
- the first leg 82 comprises in series a safing sensor 88, a squib 90 for actuating the air bag, and a crash sensor 92;
- the second leg 84 comprises in series a safing sensor 94 and a resistor 96; and
- the third leg 86 comprises in series a resistor 98 and a crash sensor 100.
- each sensor 88 and 92 is provided with a shunting resistor 102 of like nominal resistance as series resistors 96 and 98 of the second and third legs 84 and 86, respectively.
- a first diode bridge 104 comprised of oppositely biased diodes 106 connects a junction 108 on the first leg 82 between the safing sensor 88 and the squib 90 thereof (hereinafter the "first junction 108") with a junction 110 on the second leg 84 between the safing sensor 94 and the resistor 96 thereof (hereinafter the "second junction 110").
- a second diode bridge 112 comprising oppositely biased diodes 114 connects another junction 116 on the first circuit leg 82 between the squib 90 and the crash sensor 92 thereof (hereinafter the "third junction 116") with a junction 118 on the third circuit leg 86 between the resistor 98 and the crash sensor 100 thereof (hereinafter the "fourth junction 118").
- the diode bridges 104 and 112 enable either of the safing sensors 88 and 94 to "arm" both crash sensors 92 and 100.
- the current flowing through the squib 90 is increased to a value above the firing threshold thereof, whereupon the squib 90 deploys the air bag.
- the diode bridges 104 and 112 similarly provide full circuit diagnosability using the diagnostic sequence described hereinabove with respect to the first embodiment 10 of the instant firing circuit.
- the instantaneous forward-biased conduction voltage V d of each of the diodes 106 and 114 comprising the diode bridges 104 and 112 is calculated in the manner described hereinabove by alternately turning on transistors 120 and 122, the collectors of which are connected via resistors 124 to the third and fourth junctions 116 and 118 of the first and third circuit legs 82 and 86, respectively.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Air Bags (AREA)
Abstract
Description
- The instant invention relates to vehicle passenger restraint systems and, more specifically, to a firing circuit for an air bag passive restraint system which can be readily diagnosed for the presence of faults therein.
- Known air bag passenger restraint systems comprise a firing circuit having a voltage supply providing a potential across a firing squib in series with a first and second normally open vehicle acceleration sensor, each of which is shunted by a resistor of like nominal resistance. A small current thus flows through the circuit while the sensors remain in the normally open condition. The closure of the sensors upon collision or marked deceleration of the vehicle generates a significant rise in the current flowing through the squib which, in turn, fires the squib to deploy the air bag. In order to accommodate both driver and passenger air bags, a separate firing circuit is employed for each air bag, each firing independently during a vehicle collision.
- An advantage of such separate firing circuits is that the presence of a fault therein, i.e., a component failure such as the improper closure of one of the normally open sensors, is readily diagnosable by measuring the voltage potentials about the circuit. Unfortunately, since each squib is connected to only two sensors, there are no redundant fire paths for the squibs. Thus all four sensors must close in order to deploy both bags. Redundant fire paths can be created by adding additional dedicated series firing circuits for each air bag. Each air bag would thus have two or more squibs which deploy the bag upon closure of both sensors dedicated to one of the squibs, with the number of redundant fire paths therefore being equal to the number of redundant series firing circuits. Unfortunately, the resultant increase in the number of circuit elements dramatically increases both the cost of a passenger restraint system employing such circuits and the likelihood of failure of such circuit elements.
- Another known air bag firing circuit offers multiple firing paths by placing in series a first pair of normally open sensors wired in parallel, a pair of squibs wired in parallel, and a second pair of normally open sensors, also wired in parallel. The sensors are again shunted by resistors of like nominal resistance. The squibs fire upon simultaneous closure of either of the first pair of sensors and either of the second pair of sensors. The provision of multiple firing paths thus increases system reliability without the need for increasing the number of circuit elements used therein. Unfortunately, such circuits are not readily diagnosable--although the examination of voltage potentials about the circuit would indicate that a fault had occurred, there is no way to identify the precise fault, short of removing and testing each circuit element individually until the source of the fault is revealed. For example, upon the failing closed of one of the sensors comprising the first pair of sensors, both sensors must be removed and individually tested to determine which of the sensors had failed.
- It is an object of the instant invention to provide a firing circuit for a vehicle passenger restraint system having multiple firing paths while employing a minimum number of circuit elements.
- Another object of the instant invention is to provide a firing circuit for a vehicle passenger restraint system, the elements of which may be diagnosed without necessitating the disassembly of the firing circuit.
- A further object of the instant invention is to provide a method for specifically diagnosing any fault present in the instant firing circuit which does not require the disassembly thereof.
- The instant firing circuit for actuating a first and second instrumentality of a vehicle passenger restraint system, e.g., for deploying a pair of air bags, comprises first and second circuit legs connected in parallel across a voltage supply, whereby a first voltage is applied thereacross. Specifically, the first circuit leg comprises in series a first normally open sensor for detecting a first condition requiring deployment of the air bags (hereinafter "safing sensor"), a first trigger means such as a squib for deploying the first air bag having an internal resistance, and a second normally open sensor for detecting a second condition requiring deployment of the air bags (hereinafter "crash sensor"). Similarly, the second circuit leg comprises in series another safing sensor, a second squib for deploying the second air bag having an internal resistance substantially equal to the internal resistance of the first squib, and another crash sensor. Each of the normally open safing and crash sensors are shunted by a resistor having a resistance substantially greater than the internal resistance of each squib. The resistors shunting the crash and safing sensor of the first and second circuit legs, respectively, are of like nominal resistance. Alternatively, the resistors shunting the safing sensor of each circuit leg, and the resistors shunting the crash sensor of each circuit leg, respectively, are of like nominal resistance.
- A first diode bridge comprising a pair of oppositely biased diodes connects a first junction on the first circuit leg located between the safing sensor and the squib thereof with a first junction on the second circuit leg located between the safing sensor and squib thereof. Similarly, a second diode bridge comprising a pair of oppositely biased diodes connects a second junction on the first circuit leg located between the squib and crash sensor thereof with a second junction on the second circuit leg located between the squib and crash sensor thereof. The diode bridges provide multiple firing paths for the squibs, whereby both squibs are fired and, hence, both air bags are deployed, upon closure of either safing sensor and either crash sensor.
- The diode bridges additionally permit the diagnosing of the presence of a fault in the instant firing circuit in situ, as well as permitting the identification of the fault. To that end, the instant firing circuit further comprises means for reading the voltage potentials at several of the junctions thereabout and the voltage applied across the circuit legs; means for comparing the voltage potentials of the several junctions with each other; means for calculating a plurality of voltage ranges from the applied voltage and a plurality of known percentages of the applied voltage, and means for comparing the voltage potential at one of the junctions with the thus calculated voltage ranges; means for applying a second voltage across the circuit legs greater than the first applied voltage, i.e., for increasing the voltage applied thereacross, and means for comparing the voltage potential at one of the junctions upon application of the first voltage across the circuit legs with the voltage potential at the same junction when the second voltage is applied thereacross; and means for comparing the voltage drop across each of the diode bridges with the diode forward-biased conduction voltages.
- The instant firing circuit further comprises signal means for signalling the presence of the fault, and means for recording the fault, upon the diagnosis thereof. Additionally, the instant firing circuit comprises means for determining the instantaneous forward-biased conduction voltages of the diodes comprising the diode bridges, such as switchable means for drawing current from each of the circuit legs and means for calculating the resultant voltage drop across each of the diode bridges, whereby the firing circuit periodically redetermines the forward-biased conduction voltage of the diodes so as to account for manufacturing tolerances as well as the effects of time and temperature thereon.
-
- FIG. 1 is a diagrammatic schematic of an air bag firing circuit constructed in accordance with the instant invention;
- FIG. 2 is a flow chart illustrating a method for diagnosing the presence of a fault in the air bag firing circuit of FIG. 1, as executed by the microprocessor thereof;
- FIG. 3 is a flow chart illustrating a method for determining the instantaneous forward-biased conduction voltages of the diodes comprising the diode bridges of the air bag firing circuit of FIG. 1; and
- FIG. 4 is an alternate embodiment of the air bag firing circuit of the instant invention for deployment of but a single air bag and featuring multiple firing paths and full circuit diagnosability.
- Referring to FIG. 1, a
firing circuit 10 constructed in accordance with the instant invention for deploying a pair of air bags (not shown) comprises a first andsecond circuit leg DC power supply 16. TheDC power supply 16 comprises, for example, abattery 18 and acapacitor 20 connected across thebattery 18 and normally charged thereby, whereby the supply voltage Vs delivered across thecircuit legs battery 18 malfunctions or is otherwise isolated fromlegs firing circuit 10 during a vehicle collision. Alternatively, thecapacitor 20 is charged to the nominal supply voltage Vs by the pulsed output of acharging transistor 22 with the aid of aninductor 24. The input to thecharging transistor 22 comprises the pulsed output of amicroprocessor 30 which continuously monitors the output voltage Vbat of thebattery 18 and the supply voltage Vs applied across thecircuit legs diodes 32 prevent the premature discharge of thecapacitor 20. It is noted that thecapacitor 20 further serves to momentarily increase the supply voltage Vs applied across thelegs firing circuit 10 for use in diagnosing the presence of faults therein, as described hereinbelow. - The
first circuit leg 12 comprises in series a normallyopen safing sensor 34 for detecting a first condition requiring the deployment of the air bags, such as an acceleration which exceeds a first threshold value; a trigger means for deployment of the first air bag, such as afiring squib 36 therefor comprising a heating wire of nominal internal resistance which explosively deploys the first air bag when the current flowing therethrough exceeds a threshold value; and a normallyopen crash sensor 38 for detecting a second condition requiring the deployment of the air bags, such as an acceleration which exceeds a second threshold value. The second acceleration threshold of thecrash sensor 38 is higher than the first acceleration threshold of thesafing sensor 34, whereby thesafing sensor 34 effectively "arms" thecrash sensor 38, and the thusarmed crash sensor 38 fires thesquib 36 upon the acceleration of the vehicle at a rate which exceeds the second threshold value thereof. - The normally
open sensors first circuit leg 12 are each shunted by aresistor 40 of like nominal resistance. Significantly, the nominal resistance of theshunting resistors 40 is preferably several orders of magnitude larger than the nominal internal resistance of thesquib 36. For example, where the nominal internal resistance of thesquib 36 is about 2 ohms, theshunting resistors 40 preferably comprise 2k resistors. - Similarly, the
second leg 14 of thefiring circuit 10 comprises in series asecond safing sensor 42 having a like acceleration threshold as thesafing sensor 34 of thefirst circuit leg 12; asecond squib 44 having a like internal resistance as that of thefirst squib 36 for deployment of the second air bag when the current flowing there through exceeds a threshold value; and asecond crash sensor 46 having a like acceleration threshold as thecrash sensor 38 of thefirst circuit leg 12. Thesafing sensor 42 and thecrash sensor 46 of thesecond circuit leg 14 are each shunted by aresistor 48 of like nominal resistance as theshunting resistors 40 of thefirst circuit leg 12. - A
first diode bridge 50 comprising oppositelybiased diodes 52 connects ajunction 54 on thefirst leg 12 between thesafing sensor 34 and thesquib 36 thereof (hereinafter the "first junction 54") with ajunction 56 on thesecond leg 14 between thesafing sensor 42 and thesquib 44 thereof (hereinafter the "second junction 56"). Similarly, asecond diode bridge 60 comprising oppositelybiased diodes 62 connects anotherjunction 64 on thefirst circuit leg 12 between thesquib 36 and thecrash sensor 38 thereof (hereinafter the "third junction 64") with anotherjunction 66 on thesecond circuit leg 14 between thesquib 44 and thecrash sensor 46 thereof (hereinafter the "fourth junction 66"). - The
diode bridges squibs shunting resistors circuit leg squibs safing sensors crash sensors shunting resistors squibs - In accordance with another feature of the instant invention, the
diode bridges instant firing circuit 10 additionally permit the diagnosing of faults therein. More specifically, during normal operation, thefiring circuit 10 functions as a simple parallel circuit having twolegs second junctions fourth junctions circuit 10 disrupts the current flow through thelegs junctions - Accordingly, the
instant firing circuit 10 further comprises means for reading the voltage potentials at eachjunction microprocessor 30 which are connected thereto, respectively. The firingcircuit 10 further comprises a non-volatile memory unit such as anEEPROM 68 connected with themicroprocessor 30 for storing a plurality of reference values useful in diagnosing the presence of faults, and wherein the frequency and identity of such diagnosed faults are recorded for subsequent review; and signal means, such assignal lamp 70, actuated by themicroprocessor 30, whereby the presence of a fault is indicated to the vehicle operator. It is noted that, where the instantaneous voltage drop across eitherdiode bridge diodes bridge bridge bridge diodes - The diagnostic sequence executed by the
microprocessor 30 is shown schematically in FIG. 2. Specifically, the microprocessor 30 diagnoses the presence, if any, of a fault in the firing circuit 10 by: 1) reading the instantaneous supply voltage Vs and the voltage potentials at the junctions 54, 56, 64, and 66 via analog-to-digital converter ports "B", "C", "D", "E", and "F" thereon, respectively; (2) retrieving from the EEPROM 68 a plurality of range percentages previously recorded therein which define ranges of junction voltage potentials with respect to the supply voltage Vs corresponding to various groupings of possible circuit faults; (3) calculating five voltage ranges using the above percentages and the instantaneous supply voltage Vs; and (4) determining the presence and identity of any specific fault based on: (a) the voltage range in which the voltage potential V₁ at the first junction 54 lies; (b) the voltage drop V₁₂ between the first and second junctions 54 and 56 in comparison with a reference diode forward-biased conduction voltage Vd retrieved from the EEPROM 68; (c) the voltage drops between the first and third junctions 54 and 64, and the second and fourth junctions 56 and 66, respectively; and (d) the effect that charging the capacitor 20 to a voltage higher than the instantaneous supply voltage Vs used above has on the voltage potential V₁ of the first junction 54. If a fault is indicated, themicroprocessor 30 thereafter records the indicated fault in theEEPROM 68 and empowers thesignal lamp 70. It is noted that the fault range percentages may be alternately imbedded in the set of instructions to be executed by themicroprocessor 30, whereby reference need no longer be made to theEEPROM 68 to obtain such values. - The fault range percentages retrieved from the
EEPROM 68 in step (2) above are initially determined by circuit analysis in a manner known to those skilled in the art, whereby the likely change in voltage potentials at thejunctions firing circuit 10. Thus, for an exemplary embodiment of theinstant firing circuit 10 having2k shunting resistors Range 1 lies between ground and 16.5% of the supply voltage Vs;Range 2 between 16.5% and 46% of the supply voltage Vs;Range 3 between 46% and 58% of the supply voltage Vs;Range 4 between 58% and 79% of the supply voltage Vs; and Range 5 between 79% and 100% of the supply voltage Vs. Indeed, the above percentages hold true for any embodiment in which the shuntingresistors squibs - The observed voltage drops V₁₂, V₁₃, and V₂₄ developed between the first and
second junctions third junctions fourth junctions circuit 10, as indicated in the following Table, wherein "nil" represents a voltage of negligible amplitude: - The following examples serve to illustrate application of the above diagnostic sequence, as well as illustrating the use of Table I. For each example, the supply voltage Vs is 12 volts and, thus, the Ranges 1-5 as calculated under step (2) above are as follows:
Range 1, 0.0 to 1.98 volts;Range 2, 1.98 to 4.86 volts;Range 3, 4.86 to 6.88 volts;Range 4, 6.88 to 9.42 volts; and Range 5, 9.42 to 12.0 volts. It is assumed, for the following examples, that the diode forward-biased conduction voltage Vd has been found to be 0.70 volts. - The voltage potentials at the first, second, third and
fourth junctions second junctions squibs safing sensors second junctions circuit legs third junction 64 and ground, and between thefourth junction 66 and ground, respectively, (fault no. 10); or both the third and thefourth junctions firing circuit 10 are shorted to the positive terminal of the battery 18 (fault no. 11). - Further reference to Table I requires examination of the voltage drop V₁₃ between the first and
third junctions third junctions junctions - To further differentiate between fault nos. 8 and 9, the
capacitor 20 is charged by turning on chargingtransistor 22. If such charging produces an increase in the voltage potential at thefirst junction 54, then reference to Table 1 indicates that bothsafing sensors first junction 54, then the first andsecond junctions - Alternatively, the
microprocessor 30 can compare the battery voltage Vbat with the voltage potential at the first junction V₁ via analog-to-digital convertor ports "A" and "C" on themicroprocessor 30 that are connected therewith, respectively. Specifically, where the first andsecond junctions battery 18, a voltage drop substantially equal to the forward-biased conduction voltage Vd ofvoltage supply diode 32 is experienced between thebattery 18 and thefirst junction 54. Where the battery voltage Vbat is substantially equal to the voltage potential at thefirst junction 54, the first andsecond junctions battery 18, i.e., fault no. 8 is indicated. - It is noted that, where the voltage drops V₁₃ and V₂₄ are unavailable, as where the voltage potentials at only the first and
second junctions microprocessor 30, the specific fault in this example cannot be identified. Rather, the fault may only be characterized as being within two groups of faults, namely, either in the group comprising fault nos. 7, 8, and 10, or in the group comprising fault nos. 9 and 11. - The voltage potentials at the first, second, third and
fourth junctions first junction 54 is shorted to the positive terminal of the battery 18 (fault no. 1); thefirst safing sensor 34 is closed (fault no. 2); or thethird junction 64 is shorted to the positive terminal of the battery 18 (fault no. 3). Further reference to Table I using the small negative voltage drop V₁₃ present between the first andthird junctions first junction 54 is shorted to the positive terminal of the battery 18 (fault no. 1). - The voltage potentials at the first, second, third and
fourth junctions Range 3. Since the first andsecond junctions circuit 10. - The voltage potentials of the first, second, third and
fourth junctions Range 3. In as much as the voltage drop V₁₂ of -0.15 volts between the first andsecond junctions resistors circuit 10 has a nominal resistance outside of the acceptable range therefor (fault no. 17). - It is noted that, by adding an additional diode (not shown) in each
circuit leg crash sensor fourth junctions fourth junctions circuit legs - Similarly, a resistor (not shown) having a resistance substantially greater than either of the
resistors crash sensors crash sensor - It is further noted that the forward-biased conduction voltage Vd of a given diode varies both as a result of manufacturing tolerances and the operating conditions to which the diode is exposed, e.g., variations in the operating temperature thereof. Thus, in order to accurately diagnose a fault within the
firing circuit 10, the instantaneous forward-biased conduction voltage Vd of eachdiode firing circuit 10 is preferably periodically redetermined for use in the above diagnostic sequence. Accordingly, the firingcircuit 10 of the instant invention further comprises current switch means, such astransistors fourth junctions circuit legs transistor fourth junctions resistor 76 of like resistance as the shuntingresistors transistor - The method for determining the instantaneous forward-biased conduction voltages Vd of the
diodes first transistor 72 from themicroprocessor 30, thereby drawing current through theresistor 76 connected to the collectors thereof. An increased current thus flows through theleg 12 to which the empoweredtransistor 72 is connected which, in turn, results in a larger potential drop across thesafing sensor 34 thereof to provide a voltage drop across the forwardly-biased diodes of eachbridge second junctions fourth junctions microprocessor 30 via analog-to-digital convertor ports "C", "D", "E", and "F" thereon, equal the instantaneous values of the forward-biased conduction voltages of thediodes second transistor 74 drawing current from thesecond leg 14, whereby the instantaneous forward-biased conduction voltage Vd of each of the oppositely-biaseddiodes bridges diode EEPROM 68 for use in the diagnostic sequence described hereinabove. - It is noted that a preselected value for the diode forward-biased conduction voltages Vd is used if the instantaneous voltage drop across the diode cannot be calculated due to transistor or diode malfunction. In this regard, it is further noted that the diode forward-biased conduction voltages Vd can be accurately checked only when there are no faults present in the
firing circuit 10, or when the faults present fall withinRange 3, as defined hereinabove. Thus, when testing for the instantaneous diode forward-biased conduction voltage Vd, if the voltage drop V₁₂ calculated from the instantaneous voltage potentials at the first andthird junctions - The instant diagnostic sequence may additionally comprise the steps of: reading the voltage potentials V₁₂, V₁₃, V₂₃, and V₃₄ about the firing circuit several times and calculating average values therefrom for use the steps outlined hereinabove; checking the integrity of the
signal lamp 70 and empowering a back-up signal means in the event of a failure of thesignal lamp 70; signaling the specific fault detected, as by a coded sequence, via thesignal lamp 70; reading the output voltage Vs of thebattery 18 via analog-to-digital port "A" on themicroprocessor 30 and charging thecapacitor 20 if the battery voltage Vbat falls below the level sufficient to fire bothsquibs battery 18 or the isolation of thebattery 18 from thecircuit 10 during a vehicle collision; and verifying the physical attachment of theacceleration sensors - Upon the determination of the presence of a fault within the
circuit 10, themicroprocessor 30 may incorporate means therein, such as incremental counters, for determining whether the indicated fault is a system aberration, such as a momentary closure of one of thesafing sensors microprocessor 30 may further incorporate a deadman timer to ensure continued diagnostic capability therein, e.g., to cause themicroprocessor 30 to begin at a specific point in the instructions therefor in the event that themicroprocessor 30 is tied up by a random external disturbance. Themicroprocessor 30 instructions may further comprise steps for checking the integrity of theEEPROM 68 connected therewith, and for recording in theEEPROM 68 the purging of the faults recorded therein. - An
alternate embodiment 80 of the instant air bag firing circuit is illustrated in FIG. 4. The firingcircuit 80 actuates a single air bag, such as a driver's side air bag (not shown), while providing multiple firing paths and full circuit diagnosability. Specifically, the firingcircuit 80 comprises threecircuit legs voltage supply 16 similar to that described hereinabove with respect to thefirst embodiment 10 of the instant firing circuit. - The
first leg 82 comprises in series asafing sensor 88, asquib 90 for actuating the air bag, and acrash sensor 92; thesecond leg 84 comprises in series asafing sensor 94 and aresistor 96; and thethird leg 86 comprises in series aresistor 98 and acrash sensor 100. As in thefirst embodiment 10, eachsensor resistor 102 of like nominal resistance asseries resistors third legs - A
first diode bridge 104 comprised of oppositely biaseddiodes 106 connects ajunction 108 on thefirst leg 82 between thesafing sensor 88 and thesquib 90 thereof (hereinafter the "first junction 108") with ajunction 110 on thesecond leg 84 between thesafing sensor 94 and theresistor 96 thereof (hereinafter the "second junction 110"). Similarly, a second diode bridge 112 comprising oppositely biaseddiodes 114 connects anotherjunction 116 on thefirst circuit leg 82 between thesquib 90 and thecrash sensor 92 thereof (hereinafter the "third junction 116") with ajunction 118 on thethird circuit leg 86 between theresistor 98 and thecrash sensor 100 thereof (hereinafter the "fourth junction 118"). It is noted that the splitting of thesecond circuit leg 14 of thefirst embodiment 10 of the instant firing circuit into twoseparate circuit legs second embodiment 80, is necessitated by the fact that thesecond squib 44 of thefirst embodiment 10 cannot simply be replaced by a resistor of like nominal resistance upon the removal of thesecond squib 44 therefrom, as a resistor of such low nominal resistance would catastrophically fail upon the closing of a crash and safing sensor, with the attendant risk of fire or other hazard, in addition to lowering the reliability of the firing circuit. - As in the
first embodiment 10 of theinstant firing circuit 10, the diode bridges 104 and 112 enable either of thesafing sensors crash sensors safing sensors crash sensors squib 90 is increased to a value above the firing threshold thereof, whereupon thesquib 90 deploys the air bag. The diode bridges 104 and 112 similarly provide full circuit diagnosability using the diagnostic sequence described hereinabove with respect to thefirst embodiment 10 of the instant firing circuit. - The instantaneous forward-biased conduction voltage Vd of each of the
diodes transistors resistors 124 to the third andfourth junctions third circuit legs - While the preferred embodiments of the invention have been disclosed, it should be appreciated that the invention is susceptible of modification without departing from the scope of the following claims.
Claims (22)
a first circuit leg comprising in series a first normally open sensor for detecting a first condition requiring actuation of said instrumentalities, a first trigger means for actuating said first instrumentality having an internal resistance, and a second normally open sensor for detecting a second condition requiring actuation of said instrumentalities, said first and second sensor being shunted by a first and second resistor, respectively, said first and second resistors having a resistance substantially greater than the internal resistance of said first trigger means;
a second circuit leg connected in parallel with said first circuit leg comprising in series a third normally open sensor for detecting the first condition requiring actuation of said instrumentalities, a second trigger means for actuating said second instrumentality having an internal resistance substantially equal to the internal resistance of said first trigger means, and a fourth normally open sensor for detecting the second condition requiring actuation of said instrumentalities, said third and fourth sensor being shunted by a third and fourth resistor, respectively, said third and fourth resistors having a resistance substantially greater than the internal resistance of said second trigger means;
a first diode bridge comprising a pair of oppositely biased diodes connecting a first junction on said first circuit leg between said first sensor and said first trigger means with a first junction on said second circuit leg between said third sensor and second trigger means; and
a second diode bridge comprising a pair of oppositely biased diodes connecting a second junction on said first circuit leg between said first trigger means and said second sensor with a second junction on said second circuit leg between said second trigger means and said fourth sensor; and
means for applying a first voltage across said circuit legs.
means for reading the voltage potentials at a plurality of said junctions; and
means for comparing the voltage potential at one of said junctions with the voltage potential at another of said junctions.
means for reading the voltage applied across said circuit legs;
means for calculating a plurality of voltage ranges from the applied voltage and a plurality of known percentages of the applied voltage;
means for comparing the voltage potential at one of said junctions with said voltage ranges.
means for applying a second voltage across said circuit legs greater than the first applied voltage, and
means for comparing the voltage potential at one of said junctions when the first voltage is applied across said circuit legs with the voltage potential at said one of said junctions when the second voltage is applied across said circuit legs.
means for determining the forward-biased conduction voltages of the diodes comprising said diode bridges;
means for calculating the voltage drop across each of said diode bridges; and
means for comparing the voltage drop across each of said diode bridges with said diode forward-biased conduction voltages.
switchable means connected to said second junction on one of said circuit legs for drawing current therefrom;
means for reading the voltage potentials at said first and second junctions of said first circuit leg, and said first and second junctions of said second circuit leg, respectively, when said switchable means is drawing current from said leg; and
means for calculating the difference in the voltage potentials of said first and second junctions, and said third and fourth junctions, respectively, when said switchable means is drawing current from said leg.
a microprocessor having means thereon for reading the voltage potentials at a plurality of said junctions; and
a set of instructions to be executed by said microprocessor comprising the steps of
reading the voltage potentials at a plurality of the junctions on said legs through the input ports of said microprocessor, and
comparing the voltage potentials at one of said junctions with the voltage potentials at another of said junctions.
means on said microprocessor for reading said first voltage applied across said circuit legs, and
means for providing a plurality of fault range percentage values to said microprocessor;
and wherein said microprocessor instructions further comprise the steps of
reading the first voltage applied across said circuit legs,
calculating a plurality of fault voltage ranges using said fault range percentage values and said first applied voltage, and
comparing the voltage potential at one of said junctions with said fault voltage ranges.
storing the voltage potential at one of said junctions when said first voltage is applied across said circuit legs in a memory unit,
operating said means for applying said second voltage when said second voltage is applied across said circuit legs,
retrieving the voltage potential at said one of said junctions when said first voltage is applied across said circuit legs from said memory unit, and
comparing the voltage potential at said one of said junctions when said first voltage is applied across said circuit legs with the voltage potential at said one of said junctions when said second voltage is applied across said circuit legs.
a transistor, the collector of said transistor being connected to said second junction through a resistor of like nominal resistance as said shunting resistors of said leg, the emitter of said transistor being connected to location on said circuit leg having a zero voltage potential; and
means for switchably delivering a current to the base of said transistor.
a first circuit leg comprising in series a first normally open sensor for detecting a first condition requiring actuation of said instrumentalities, trigger means for actuating said instrumentality having an internal resistance, and a second normally open sensor for detecting a second condition requiring actuation of said instrumentalities, said first and second sensor being shunted by a first and second resistor, respectively, having a resistance substantially greater than the internal resistance of said trigger means;
a second circuit leg connected in parallel with said first circuit leg comprising in series a third normally open sensor for detecting the first condition requiring actuation of said instrumentalities and a third resistor having a resistance substantially greater than the internal resistance of said trigger means;
a third circuit leg connected in parallel with said first and second circuit legs comprising in series a fourth resistor and a fourth normally open sensor for detecting the second condition requiring actuation of said instrumentality, said fourth resistor having a resistance substantially greater than the resistance of said trigger means;
a first diode bridge comprising a pair of oppositely biased diodes connecting a first junction on said first circuit leg between said first sensor and said trigger means with a junction on said second circuit leg between said third sensor and said third resistor; and
a second diode bridge comprising a pair of oppositely biased diodes connecting a second junction on said first circuit leg between said first trigger means and said second sensor thereof with a junction on said third circuit leg between said fourth resistor and said fourth sensor; and
means for applying a first voltage across said circuit legs.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/249,366 US4851705A (en) | 1988-09-23 | 1988-09-23 | Firing circuit for a vehicle passenger restraint system |
US249366 | 1988-09-23 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0360376A2 true EP0360376A2 (en) | 1990-03-28 |
EP0360376A3 EP0360376A3 (en) | 1990-07-18 |
EP0360376B1 EP0360376B1 (en) | 1993-08-25 |
Family
ID=22943163
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP89304475A Expired - Lifetime EP0360376B1 (en) | 1988-09-23 | 1989-05-04 | Firing circuit for a vehicle passenger restraint system |
Country Status (8)
Country | Link |
---|---|
US (1) | US4851705A (en) |
EP (1) | EP0360376B1 (en) |
JP (1) | JPH0657521B2 (en) |
KR (1) | KR920007863B1 (en) |
AU (1) | AU605989B2 (en) |
CA (1) | CA1336723C (en) |
DE (1) | DE68908649T2 (en) |
ES (1) | ES2045424T3 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1992005980A2 (en) * | 1990-09-27 | 1992-04-16 | Trw Inc. | Method and apparatus for testing a dual airbag passive restraint system |
WO1996021263A1 (en) * | 1994-12-30 | 1996-07-11 | Robert Bosch Gmbh | Electronic device |
DE10062756A1 (en) * | 2000-12-15 | 2002-06-20 | Conti Temic Microelectronic | Circuit arrangement for controlling a gas generator of an occupant protection device which can be influenced by a magnetic field in the course of the ignition |
EP1594021A1 (en) * | 2004-05-05 | 2005-11-09 | Siemens Aktiengesellschaft | Circuit device and method for testing relay switching contacts of a digital output circuit |
DE19542085B4 (en) * | 1994-12-30 | 2007-07-05 | Robert Bosch Gmbh | Safety device for vehicle occupants |
Families Citing this family (51)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5571994A (en) * | 1988-05-04 | 1996-11-05 | Norton; Peter | Weatherproof seal for wire entrance |
JPH05459Y2 (en) * | 1988-05-11 | 1993-01-07 | ||
JPH0735142B2 (en) * | 1988-05-24 | 1995-04-19 | 日本電装株式会社 | Failure determination device for vehicle occupant protection system |
DE3829784A1 (en) * | 1988-09-02 | 1990-03-15 | Bosch Gmbh Robert | EVALUATION PROCESS FOR SENSOR OUTPUT SIGNALS |
US5231253A (en) * | 1989-02-23 | 1993-07-27 | Automotive Technologies, International | Side impact sensors |
US4979763A (en) * | 1989-05-30 | 1990-12-25 | Trw Vehicle Safety Systems Inc. | Method and apparatus for sensing a vehicle crash |
US5668723A (en) * | 1989-05-30 | 1997-09-16 | Trw Vehicle Safety Systems Inc. | Method and apparatus for sensing a vehicle crash using crash energy |
JP2826839B2 (en) * | 1989-06-15 | 1998-11-18 | アスコ株式会社 | Control circuit of vehicle safety device |
DE3922506A1 (en) * | 1989-07-08 | 1991-01-17 | Bosch Gmbh Robert | VEHICLE VEHICLE SAFETY SYSTEM |
US4980573A (en) * | 1989-10-02 | 1990-12-25 | Automotive Systems Laboratory, Inc. | Firing circuit with three crash sensors |
US4987316A (en) * | 1989-10-03 | 1991-01-22 | Automotive Systems Laboratory, Inc. | Passenger restraint firing circuit |
DE4031327A1 (en) * | 1989-10-06 | 1991-04-11 | Breed Automotive Tech | ACCELERATION SENSOR, IN PARTICULAR FOR Passenger Restraint Systems In A VEHICLE |
US5322325A (en) * | 1989-10-19 | 1994-06-21 | Breed Automotive Technology, Inc. | Safing velocity change sensor |
US5021678A (en) * | 1989-11-03 | 1991-06-04 | Trw Technar Inc. | Apparatus and method for actuating a passenger restraint system in a passenger vehicle |
US5109341A (en) * | 1989-11-03 | 1992-04-28 | Trw Vehicle Safety Systems Inc. | Method and apparatus for sensing a vehicle crash in the frequency domain |
JP2698454B2 (en) * | 1989-11-14 | 1998-01-19 | アスコ株式会社 | Detector control circuit |
US5217252A (en) * | 1990-04-17 | 1993-06-08 | Kabushiki Kaisha Tokai-Rika-Denki-Seisakusho | Actuator for use in emergency situation of vehicle |
US5085464A (en) * | 1990-11-14 | 1992-02-04 | Automotive Systems Laboratory, Inc. | Air bag firing circuit |
JPH0818529B2 (en) * | 1990-11-20 | 1996-02-28 | 三菱電機株式会社 | Occupant protection device failure detection device |
US5099762A (en) * | 1990-12-05 | 1992-03-31 | Special Devices, Incorporated | Electrostatic discharge immune electric initiator |
US5293153A (en) * | 1991-04-09 | 1994-03-08 | Trw, Inc. | Method and apparatus for testing an airbag restraint system with parallel sensors |
US5261694A (en) * | 1991-06-14 | 1993-11-16 | Automotive Systems Laboratory, Inc. | Reconfigurable air bag firing circuit |
US6419265B1 (en) | 1993-09-16 | 2002-07-16 | Automotive Technologies International Inc. | Self-contained airbag system |
US6685218B1 (en) * | 1993-09-16 | 2004-02-03 | Automotive Technologies International, Inc. | Side impact sensors and airbag system |
GB2259616B (en) * | 1991-07-25 | 1995-07-05 | Autoliv Dev | Improvements in or relating to an ignition circuit for an air-bag |
JP2876363B2 (en) * | 1991-09-11 | 1999-03-31 | トヨタ自動車株式会社 | Side impact sensor system for side airbag device |
DE59301479D1 (en) * | 1992-03-12 | 1996-02-29 | Siemens Ag | TRIP CIRCUIT OF A CRASH SENSOR-CONTROLLED PROTECTION SYSTEM OF A VEHICLE |
US5447051A (en) * | 1993-08-05 | 1995-09-05 | Hewlett-Packard Company | Method and apparatus for testing a piezoelectric force sensor |
JP2661863B2 (en) * | 1993-10-29 | 1997-10-08 | 富士通テン株式会社 | Squib line diagnostic device for airbag system of vehicle |
US5496979A (en) * | 1994-03-11 | 1996-03-05 | Automotive Systems Laboratory, Inc. | Accelerometer with optical switch |
US5656991A (en) * | 1995-05-22 | 1997-08-12 | Trw Inc. | Apparatus for testing an actuatable restraint system |
US8229624B2 (en) * | 1995-06-07 | 2012-07-24 | American Vehicular Sciences Llc | Vehicle diagnostic information generating and transmission systems and methods |
US8157047B2 (en) * | 1995-06-07 | 2012-04-17 | Automotive Technologies International, Inc. | Occupant protection systems control techniques |
US20080046149A1 (en) * | 1995-06-07 | 2008-02-21 | Automotive Technologies International, Inc. | Vehicle Component Control Methods and Systems Based on Vehicle Stability |
US7650210B2 (en) * | 1995-06-07 | 2010-01-19 | Automotive Technologies International, Inc. | Remote vehicle diagnostic management |
US8060282B2 (en) * | 1995-06-07 | 2011-11-15 | Automotive Technologies International, Inc. | Vehicle component control methods and systems based on vehicle stability |
US20080161989A1 (en) * | 1995-06-07 | 2008-07-03 | Automotive Technologies International, Inc. | Vehicle Diagnostic or Prognostic Message Transmission Systems and Methods |
US8019501B2 (en) * | 1995-06-07 | 2011-09-13 | Automotive Technologies International, Inc. | Vehicle diagnostic and prognostic methods and systems |
US8036788B2 (en) * | 1995-06-07 | 2011-10-11 | Automotive Technologies International, Inc. | Vehicle diagnostic or prognostic message transmission systems and methods |
US20080147280A1 (en) * | 1995-06-07 | 2008-06-19 | Automotive Technologies International, Inc. | Method and apparatus for sensing a rollover |
US20050184496A1 (en) | 2003-10-03 | 2005-08-25 | Speckhart Frank H. | Sensor pad for controlling airbag deployment and associated support |
US6095553A (en) * | 1998-06-30 | 2000-08-01 | Ford Global Technologies, Inc. | Side impact sensor system and method |
US6311162B1 (en) * | 1998-07-25 | 2001-10-30 | Ernst F. Reichwein | Interactive symptomatic recording system and methods |
US6124784A (en) * | 1998-08-11 | 2000-09-26 | Trw Inc. | Occupant protection and signal apparatus and method |
DE19955551A1 (en) * | 1998-11-19 | 2000-05-25 | Inova Gmbh Tech Entwicklungen | Airbag arrangement has switch operated depending on correct spreading of gas bag as a result of inflation by preceding gas generation stage to switch next stage electrically/electronically |
US7158870B2 (en) * | 2002-01-24 | 2007-01-02 | Ford Global Technologies, Llc | Post collision restraints control module |
US20060045751A1 (en) * | 2004-08-30 | 2006-03-02 | Powermate Corporation | Air compressor with variable speed motor |
TW200906657A (en) * | 2007-08-07 | 2009-02-16 | Univ Southern Taiwan Tech | Safety device for preventing fuel leakage |
DE102008028726A1 (en) * | 2007-09-27 | 2009-04-02 | C. Rob. Hammerstein Gmbh & Co. Kg | Adjusting device for adjusting head rest of motor vehicle seat, has crash sensor emitting signal during excess voltage in driving condition, where excess voltage amounts to specific percentage of value of normal operating voltage |
US9279406B2 (en) | 2012-06-22 | 2016-03-08 | Illinois Tool Works, Inc. | System and method for analyzing carbon build up in an engine |
US9283912B2 (en) * | 2013-06-27 | 2016-03-15 | Zodiac Cabin Controls Gmbh | Airbag control unit |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3633159A (en) * | 1970-11-10 | 1972-01-04 | Gen Motors Corp | Vehicle air cushion actuation and monitoring circuit |
US4086562A (en) * | 1975-02-17 | 1978-04-25 | Hitachi, Ltd. | Apparatus for recording erroneous operations of passenger protecting apparatus for motor vehicles |
DE3116867A1 (en) * | 1981-04-28 | 1982-11-11 | Bayerische Motoren Werke AG, 8000 München | Switching arrangement for actuating emergency functions in motor vehicles |
US4366465A (en) * | 1981-10-02 | 1982-12-28 | Ford Motor Company | False failure detection prevention in an air bag diagnostic system |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3921129A (en) * | 1971-05-10 | 1975-11-18 | Toyo Kogyo Co | Malfunction preventive system for use in an air bag incorporating a sensor for detecting the collision speed of a vehicle |
JPS5327933A (en) * | 1976-08-24 | 1978-03-15 | Honda Motor Co Ltd | Automotive air-bag activating apparatus |
DE2745620A1 (en) * | 1977-10-11 | 1979-04-12 | Daimler Benz Ag | AIR BAG SYSTEM TO PROTECT THE OCCUPANTS OF A MOTOR VEHICLE IN THE EVENT OF ACCIDENTS |
FR2467740A1 (en) * | 1979-10-23 | 1981-04-30 | Renault | SYSTEM FOR DETECTING COLLISIONS AND CONTROLLING A SAFETY DEVICE |
JPS6243877Y2 (en) * | 1980-03-25 | 1987-11-16 | ||
JPS5766050A (en) * | 1980-10-02 | 1982-04-22 | Nippon Denso Co Ltd | Mesexplosion recording device of air bag device |
DE3326277A1 (en) * | 1983-07-21 | 1985-01-31 | Robert Bosch Gmbh, 7000 Stuttgart | AT LEAST FOUR TRIGGER CIRCUIT RELEASE DEVICE OF A VEHICLE occupant protection device |
JPH0323892Y2 (en) * | 1984-10-16 | 1991-05-24 | ||
EP0284770B2 (en) * | 1987-03-26 | 1993-03-24 | Siemens Aktiengesellschaft | Control circuit for protection device |
-
1988
- 1988-09-23 US US07/249,366 patent/US4851705A/en not_active Expired - Lifetime
-
1989
- 1989-05-04 CA CA000598736A patent/CA1336723C/en not_active Expired - Fee Related
- 1989-05-04 ES ES89304475T patent/ES2045424T3/en not_active Expired - Lifetime
- 1989-05-04 DE DE89304475T patent/DE68908649T2/en not_active Expired - Fee Related
- 1989-05-04 EP EP89304475A patent/EP0360376B1/en not_active Expired - Lifetime
- 1989-06-15 JP JP1150698A patent/JPH0657521B2/en not_active Expired - Lifetime
- 1989-07-06 AU AU37921/89A patent/AU605989B2/en not_active Ceased
- 1989-07-19 KR KR1019890010228A patent/KR920007863B1/en not_active IP Right Cessation
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3633159A (en) * | 1970-11-10 | 1972-01-04 | Gen Motors Corp | Vehicle air cushion actuation and monitoring circuit |
US4086562A (en) * | 1975-02-17 | 1978-04-25 | Hitachi, Ltd. | Apparatus for recording erroneous operations of passenger protecting apparatus for motor vehicles |
DE3116867A1 (en) * | 1981-04-28 | 1982-11-11 | Bayerische Motoren Werke AG, 8000 München | Switching arrangement for actuating emergency functions in motor vehicles |
US4366465A (en) * | 1981-10-02 | 1982-12-28 | Ford Motor Company | False failure detection prevention in an air bag diagnostic system |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1992005980A2 (en) * | 1990-09-27 | 1992-04-16 | Trw Inc. | Method and apparatus for testing a dual airbag passive restraint system |
WO1992005980A3 (en) * | 1990-09-27 | 1993-02-18 | Trw Inc | Method and apparatus for testing a dual airbag passive restraint system |
WO1996021263A1 (en) * | 1994-12-30 | 1996-07-11 | Robert Bosch Gmbh | Electronic device |
DE19542085B4 (en) * | 1994-12-30 | 2007-07-05 | Robert Bosch Gmbh | Safety device for vehicle occupants |
DE10062756A1 (en) * | 2000-12-15 | 2002-06-20 | Conti Temic Microelectronic | Circuit arrangement for controlling a gas generator of an occupant protection device which can be influenced by a magnetic field in the course of the ignition |
US6564717B2 (en) | 2000-12-15 | 2003-05-20 | Conti Temic Microelectronic Gmbh | Circuit arrangement for driving an occupant protection system gas generator whose ignition process can be influenced by a magnetic field |
EP1594021A1 (en) * | 2004-05-05 | 2005-11-09 | Siemens Aktiengesellschaft | Circuit device and method for testing relay switching contacts of a digital output circuit |
Also Published As
Publication number | Publication date |
---|---|
ES2045424T3 (en) | 1994-01-16 |
KR920007863B1 (en) | 1992-09-18 |
US4851705A (en) | 1989-07-25 |
AU3792189A (en) | 1990-03-29 |
KR900004559A (en) | 1990-04-12 |
AU605989B2 (en) | 1991-01-24 |
DE68908649D1 (en) | 1993-09-30 |
EP0360376B1 (en) | 1993-08-25 |
EP0360376A3 (en) | 1990-07-18 |
DE68908649T2 (en) | 1993-12-23 |
JPH0288344A (en) | 1990-03-28 |
CA1336723C (en) | 1995-08-15 |
JPH0657521B2 (en) | 1994-08-03 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0360376B1 (en) | Firing circuit for a vehicle passenger restraint system | |
US4980573A (en) | Firing circuit with three crash sensors | |
US4987316A (en) | Passenger restraint firing circuit | |
US5187465A (en) | Method and apparatus for testing a dual airbag passive restraint system | |
EP0396265B1 (en) | Air bag firing circuit | |
US4893109A (en) | Airbag electrical igniter readiness detector | |
JP3688296B2 (en) | Electronic safety device for vehicle passengers | |
EP0535207B1 (en) | Method and apparatus for testing an airbag restraint system with parallel sensors | |
EP0386012B1 (en) | Triggering circuit for a vehicle air bag | |
US5136275A (en) | Ground connection monitoring for airbag electrical igniter circuit | |
USH2094H1 (en) | Diagnostic circuit for vehicle device control module | |
JPH0270550A (en) | Data extraction |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): DE ES FR GB IT |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
RHK1 | Main classification (correction) |
Ipc: B60R 21/00 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): DE ES FR GB IT |
|
17P | Request for examination filed |
Effective date: 19900730 |
|
17Q | First examination report despatched |
Effective date: 19920124 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE ES FR GB IT |
|
REF | Corresponds to: |
Ref document number: 68908649 Country of ref document: DE Date of ref document: 19930930 |
|
ET | Fr: translation filed | ||
ITF | It: translation for a ep patent filed | ||
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2045424 Country of ref document: ES Kind code of ref document: T3 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19940505 |
|
ITTA | It: last paid annual fee | ||
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 19980511 Year of fee payment: 10 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20000131 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20000502 Year of fee payment: 12 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20000503 Year of fee payment: 12 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20000503 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20010504 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20010504 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20020301 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20050504 |